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Accession Number:
AD0607654
Title:
SEVERAL MODELS OF SIX DEGREE OF FREEDOM EQUATIONS OF MOTION FOR A BALLISTIC MISSILE
Corporate Author:
CHRYSLER CORP DETROIT MI MISSILE DIV
Report Date:
1962-03-06
Abstract:
Presented in this report are total and perturbation six degree of freedom equations of motion and their derivations. Magnus force and moment were considered negligible and not included in this derivation, however, when desired they can be incorporated in the existing models. Definitions of control force, gravity, thrust and damping terms are presented in general form so that various control schemes and particular functions of the terms can be utilized without extensive modification to the equations of motion. These equations may be programmed on a large scale digital or analog computer. Author
Supplementary Note:
Legibility of this document is in part unsatisfactory. Reproduction has been made from best available copy DOI: 10.21236/AD0607654
Pages:
0054
Contract Number:
AF 04(694)-25
File Size:
1.36MB
